Pt. 121, App. M 14 CFR Ch. I (1-1-19 Edition) The recorded values must meet the designated range, resolution and accuracy requirements during static and dynamic conditions. Dynamic condition means the parameter is experiencing change at the maximum rate attainable, including the maximum rate of reversal. All data recorded must be correlated in time to within one second. Parameters Range Accuracy (sensor input) Seconds per sampling interval 42. Throttle/power Leverl position. 16. 43. Additional Engine Parameters. Full Range ......... Section2% ................... 1 for each lever 2% of full range As installed ........ As installed ........ Each engine each second. 2% of full range 44. Traffic Alert and Collision Avoidance System (TCAS). Discretes ........... As installed ........ 1 ........................ ........................... 45. DME 1 and 2 Distance. 46. Nav 1 and 2 Selected Frequency. 47. Selected barometric setting. 48. Selected Altitude. 49. Selected speed. 50. Selected Mach. 51. Selected vertical speed. 52. Selected heading. 53. Selected flight path. 54. Selected decision height. 55. EFIS display format. 0-200 NM ......... As installed ........ 4 ........................ 1 NM ................. Full Range ......... As installed ........ 4 ........................ ........................... Full Range ......... Section5% ................... (1 per 64 sec.) .. Full Range ......... Section5% ................... 1 ........................ 0.2% of full range 100 ft Full Range ......... Section5% ................... 1 ........................ 1 knot Full Range ......... Section5% ................... 1 ........................ .01 Full Range ......... Section5% ................... 1 ........................ 100 ft/min Full Range ......... Section5% ................... 1 ........................ 1Section Full Range ......... Section5% ................... 1 ........................ 1Section Full Range ......... Section5% ................... 64 ...................... 1 ft Discrete(s) ......... ........................... 4 ........................ ........................... 56. Multi-function/ Engine Alerts Display format. Discrete(s) ......... ........................... 4 ........................ ........................... 57. Thrust command. 17. 58. Thrust target 59. Fuel quantity in CG trim tank. 60. Primary Navigation System Reference. Full Range ......... Section2% ................... 2 ........................ 2% of full range. Full Range ......... Full Range ......... Section2% ................... Section5% ................... 4 ........................ (1 per 64 sec.) .. 2% of full range 1% of full range Discrete GPS, INS, VOR/ DME, MLS, Localizer Glideslope. Discrete - ice - or - no ice - . Discrete ............. ........................... 4 ........................ ........................... ........................... 4 ........................... 1 61. Ice Detection 62. Engine warning each engine vibration. Resolution Remarks For airplanes with non-mechanically linked cockpit engine controls. Where capacity permits, the preferred priority is indicated vibration level, N2, EGT, Fuel Flow, Fuel Cutoff lever position and N3, unless engine manufacturer recommends otherwise. A suitable combination of discretes should be recorded to determine the status of - Combined Control, Vertical Control, Up Advisory, and Down Advisory. (ref. ARINC Characteristic 735 Attachment 6E, TCAS VERTICAL RA DATA OUTPUT WORD.) 1 mile Sufficient to determine selected frequency Discretes should show the display system status (e.g., off, normal, fail, composite, sector, plan, nav aids, weather radar, range, copy. Discretes should show the display system status (e.g., off, normal, fail, and the identity of display pages for emergency procedures, need not be recorded. A suitable combination of discretes to determine the Primary Navigation System reference. 302 VerDate Sep<11>2014 08:20 May 17, 2019 Jkt 247048 PO 00000 Frm 00312 Fmt 8010 Sfmt 8002 Y:\SGML\247048.XXX 247048